The reservoir pressure and temperature for a Laval nozzle are 5 atm [abs] and 520 K, respectively. The flow is isentropically expanded to supersonic speed at the nozzle exit with area A = 4in². If the exit-to-throat area ratio is 2.295, calculate the following exit properties:
a) Me;
b) pe;
c) Te;
d) pe;
e) po,e;
f) To,e;
g) m.